View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 25407U 98045B 25196.73661986 .00000290 00000-0 17066-3 0 9997
2 25407 71.0127 319.8632 0006804 10.5795 349.5470 14.16144876393554
Epoch (UTC): | 15 July 2025 17:40:43 |
Eccentricity: | 0.0006804 |
inclination: | 71.0127° |
perigee height: | 833 km |
apogee height: | 843 km |
right ascension of ascending node: | 319.8632° |
argument of perigee: | 10.5795° |
revolutions per day: | 14.16144876 |
mean anomaly at epoch: | 349.5470° |
orbit number at epoch: | 39355 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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